US20110243728A1 - Blower designed for fitting particularly in a chamber furnace - Google Patents
Blower designed for fitting particularly in a chamber furnace Download PDFInfo
- Publication number
- US20110243728A1 US20110243728A1 US12/662,146 US66214610A US2011243728A1 US 20110243728 A1 US20110243728 A1 US 20110243728A1 US 66214610 A US66214610 A US 66214610A US 2011243728 A1 US2011243728 A1 US 2011243728A1
- Authority
- US
- United States
- Prior art keywords
- rotor wheel
- diameter
- inlet
- blower
- chamber furnace
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 239000007787 solid Substances 0.000 claims abstract description 4
- 239000003795 chemical substances by application Substances 0.000 description 9
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001186 cumulative effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
Definitions
- This invention relates to a blower designed for fitting in a chamber furnace in particular and used, among others, in furnaces for annealing of aluminium sheet.
- blowers In furnaces requiring circulation of hot gases, usually radial or axial blowers are used. The fitting of the latter is subject to significant restrictions that affect their operating parameters. Due to the conditions of the bearings operation, the blowers are usually built as overhung. In order to avoid excessive overhang and unnecessary increase of the furnace chamber size, rotor wheels are fitted close to the chamber wall. This is also the reason for insufficient space for the stationary airfoils, which, in turn, considerably affects the efficiency and flow parameters of the axial blower. Therefore, the parameters of such blowers do not usually exceed the value of pressure difference ⁇ equalling 0.2 and the value of flow ⁇ equalling 0.3.
- the invented blower particularly the one to be fitted in a chamber furnace, in the form of a rotor wheel with blades set diagonally on the shaft, set in an enclosure creating an inlet confuser duct, with its bridge with an approximate angle of 90° behind the rotor wheel, which turns smoothly into a radial diffuser, behind which it has a bridge shaped with an approximate angle of 90° ending with a nozzle box with nozzles
- the hub of the rotor wheel has the shape of a solid of revolution with its slant height described by n degree polynomial and its Dp 2 outlet diameter greater than Dp 1 inlet diameter and the outward diameter of the axial and radial rotor wheel with spatially shaped blades monotonically increasing towards the flow from D 1 z inlet diameter to D 2 z outlet diameter.
- the presented solution owing to the shape of the rotor allowing the shaping of the first bridge with a large angle, will enable an increase in the circulation efficiency and, at the same time, maintain the required thermodynamic parameters.
- FIG. 1 presents a cross-section of the blower on the plane passing through its longitudinal axis and bridge axis, whereas
- FIG. 2 presents a cross-section of the hub and the blade of the rotor wheel.
- the blower shaft 1 there is a diagonally set rotor wheel 3 with spatially shaped blades 4 .
- the wheel 3 is set in the enclosure 5 , creating the inlet confuser duct 6 .
- Behind the rotor wheel 3 the blower has a bridge 7 with an approximate angle of 90°, which turns smoothly into a radial diffuser 8 , behind which there is another bridge 9 with an approximate angle of 90°, ending with a nozzle box 10 with nozzles 11 .
- the hub 12 of the rotor wheel 3 has the shape of a solid of revolution with its slant height described by n degree polynomial, with its Dp 2 outlet diameter greater than Dp 1 inlet diameter and the outward diameter of the axial and radial rotor wheel 3 with spatially shaped blades 4 , monotonically increasing towards the flow from D 1 z inlet diameter to D 2 z outlet diameter.
- the rotor wheel 3 is a semi-open wheel without a cover. Between the external contours of the blades 4 and the stationary body of the blower there is gap ⁇ , the size of which depends on mutual thermal dilatation of the wheel 3 and the body. It is also possible to deliver a blower, in which the wheel structure 3 is equipped with a cover.
- the hot air or other gas flows through the stationary duct 6 , gaining acceleration of several percent, which favours levelling of the velocity profile on the inlet surface of the rotor wheel 3 .
- the direction of the flow of the agent onto the blades 4 of the rotor wheel 3 is approximately axial.
- the agent flows through the system of blades 4 of the rotor wheel 3 , which conveys energy to the agent in accordance with the basic equation for fluid flow machines (Euler's identity).
- the agent is subject to compression.
- the degree of compression depends upon a selection of geometrical parameters of the rotor wheel 3 and its rotating velocity.
- the agent leaves the rotor wheel 3 at an angle in relation to the rotor rotation axis 3 —diagonally.
- the ⁇ flow-out angle on the meridional plane is described by ⁇ relation ⁇ 90°.
- the flow-out angle for the agent leaving the rotor wheel 3 depends on the assumed angle of the blade at the outlet and assumed rotating velocity.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The blower designed particularly for fitting in a chamber furnace has the hub of the rotor wheel in the shape of a solid of revolution with its slant height described by n degree polynomial and its Dp2 outlet diameter greater than Dp1 inlet diameter and the outward diameter of the axial and radial rotor wheel with spatially shaped blades monotonically increasing towards the flow from D1 z inlet diameter to D2 z outlet diameter.
Description
- This invention relates to a blower designed for fitting in a chamber furnace in particular and used, among others, in furnaces for annealing of aluminium sheet.
- In furnaces requiring circulation of hot gases, usually radial or axial blowers are used. The fitting of the latter is subject to significant restrictions that affect their operating parameters. Due to the conditions of the bearings operation, the blowers are usually built as overhung. In order to avoid excessive overhang and unnecessary increase of the furnace chamber size, rotor wheels are fitted close to the chamber wall. This is also the reason for insufficient space for the stationary airfoils, which, in turn, considerably affects the efficiency and flow parameters of the axial blower. Therefore, the parameters of such blowers do not usually exceed the value of pressure difference Ψ equalling 0.2 and the value of flow ψ equalling 0.3.
- As compared to axial blowers, radial blowers used in furnaces ensure considerably greater pressure increments (with Ψ pressure difference exceeding 0.4) however they are burdened with significant defects. First of all, in order to achieve the required pressure increment, the dynamic pressure should be recovered in a reasonably efficient manner. In classic designs of blowers this is done in cumulative spirals with large angles of wrap, i.e. up to 360°. In chamber furnaces, air exhausted from the blower must go in two opposite ways. The use of one or two exhaust spirals is very difficult for structural reasons. In practice this results in an unequal distribution of velocities on both exhaust surfaces of the blower, which is even magnified by existence of a considerable angular momentum of the agent behind the rotor wheel. Such defects are typical of radial and drum blowers.
- The description of the patent No. DE 10022788 presents a solution involving a use of an axial rotor with a constant outward diameter cooperating with two flat diffusers turning into two nozzle boxes. This blower is characterised by the same flow parameters as typical axial blowers, however, it shows much greater pressure increments and ensures an equal flow of the agent in both ways. Additionally, such blowers do not require using additional stators for the purposes of levelling of the field of velocity. However, the circulation efficiency of such blowers is relatively low (0.4). One of the reasons for such a low circulation efficiency is the fact that the agent leaving the axial rotor has a great kinetic energy and, therefore, losses generated in the bridge at the angle of 90° are also considerable, as diffusers operate with a rotational stall at the outlet.
- The invented blower, particularly the one to be fitted in a chamber furnace, in the form of a rotor wheel with blades set diagonally on the shaft, set in an enclosure creating an inlet confuser duct, with its bridge with an approximate angle of 90° behind the rotor wheel, which turns smoothly into a radial diffuser, behind which it has a bridge shaped with an approximate angle of 90° ending with a nozzle box with nozzles is characterised in that the hub of the rotor wheel has the shape of a solid of revolution with its slant height described by n degree polynomial and its Dp2 outlet diameter greater than Dp1 inlet diameter and the outward diameter of the axial and radial rotor wheel with spatially shaped blades monotonically increasing towards the flow from D1 z inlet diameter to D2 z outlet diameter.
- The presented solution, owing to the shape of the rotor allowing the shaping of the first bridge with a large angle, will enable an increase in the circulation efficiency and, at the same time, maintain the required thermodynamic parameters.
- The invention will be shown on an exemplary drawing, which does not restrict its construction as shown in the drawing, in which
FIG. 1 presents a cross-section of the blower on the plane passing through its longitudinal axis and bridge axis, whereas -
FIG. 2 presents a cross-section of the hub and the blade of the rotor wheel. - On the blower shaft 1 there is a diagonally set
rotor wheel 3 with spatially shaped blades 4. Thewheel 3 is set in theenclosure 5, creating the inlet confuser duct 6. Behind therotor wheel 3 the blower has a bridge 7 with an approximate angle of 90°, which turns smoothly into aradial diffuser 8, behind which there is another bridge 9 with an approximate angle of 90°, ending with a nozzle box 10 with nozzles 11. Thehub 12 of therotor wheel 3 has the shape of a solid of revolution with its slant height described by n degree polynomial, with its Dp2 outlet diameter greater than Dp1 inlet diameter and the outward diameter of the axial andradial rotor wheel 3 with spatially shaped blades 4, monotonically increasing towards the flow from D1 z inlet diameter to D2 z outlet diameter. Therotor wheel 3 is a semi-open wheel without a cover. Between the external contours of the blades 4 and the stationary body of the blower there is gap δ, the size of which depends on mutual thermal dilatation of thewheel 3 and the body. It is also possible to deliver a blower, in which thewheel structure 3 is equipped with a cover. - The hot air or other gas flows through the stationary duct 6, gaining acceleration of several percent, which favours levelling of the velocity profile on the inlet surface of the
rotor wheel 3. The direction of the flow of the agent onto the blades 4 of therotor wheel 3 is approximately axial. Next, the agent flows through the system of blades 4 of therotor wheel 3, which conveys energy to the agent in accordance with the basic equation for fluid flow machines (Euler's identity). The agent is subject to compression. The degree of compression depends upon a selection of geometrical parameters of therotor wheel 3 and its rotating velocity. The agent leaves therotor wheel 3 at an angle in relation to therotor rotation axis 3—diagonally. The γ flow-out angle on the meridional plane is described by γ relation <90°. The flow-out angle for the agent leaving therotor wheel 3 depends on the assumed angle of the blade at the outlet and assumed rotating velocity.
Claims (1)
1. The blower designed particularly for fitting in a chamber furnace, in the form of a rotor wheel with blades set diagonally on the shaft, set in an enclosure creating an inlet confuser duct, with its bridge with an approximate angle of 90° behind the rotor wheel, which turns smoothly into a radial diffuser, behind which it has a bridge shaped with an approximate angle of 90° ending with a nozzle box with nozzles wherein the hub of the rotor wheel has the shape of a solid of revolution with its slant height described by n degree polynomial and its Dp2 outlet diameter greater than Dp1 inlet diameter and the outward diameter of the axial and radial rotor wheel with spatially shaped blades monotonically increasing towards the flow from D1 z inlet diameter to D2 z outlet diameter.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/662,146 US20110243728A1 (en) | 2010-04-01 | 2010-04-01 | Blower designed for fitting particularly in a chamber furnace |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/662,146 US20110243728A1 (en) | 2010-04-01 | 2010-04-01 | Blower designed for fitting particularly in a chamber furnace |
Publications (1)
Publication Number | Publication Date |
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US20110243728A1 true US20110243728A1 (en) | 2011-10-06 |
Family
ID=44709891
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/662,146 Abandoned US20110243728A1 (en) | 2010-04-01 | 2010-04-01 | Blower designed for fitting particularly in a chamber furnace |
Country Status (1)
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US (1) | US20110243728A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109214141A (en) * | 2018-11-20 | 2019-01-15 | 西华大学 | Rotating stall prediction method and device |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3028140A (en) * | 1957-06-17 | 1962-04-03 | James R Lage | Rotary fluid flow machine having rotor vanes constructed according to three dimensional calculations |
US3904308A (en) * | 1973-05-16 | 1975-09-09 | Onera (Off Nat Aerospatiale) | Supersonic centrifugal compressors |
DE10022788A1 (en) * | 2000-05-10 | 2001-11-22 | Ingenieurgemeinschaft Wsp Prof | Hot gas ventilator for industrial oven; has semi-axial impeller enclosed directly by ninety degree deflector to guide volume flow from impeller radially away from impeller axis |
-
2010
- 2010-04-01 US US12/662,146 patent/US20110243728A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3028140A (en) * | 1957-06-17 | 1962-04-03 | James R Lage | Rotary fluid flow machine having rotor vanes constructed according to three dimensional calculations |
US3904308A (en) * | 1973-05-16 | 1975-09-09 | Onera (Off Nat Aerospatiale) | Supersonic centrifugal compressors |
DE10022788A1 (en) * | 2000-05-10 | 2001-11-22 | Ingenieurgemeinschaft Wsp Prof | Hot gas ventilator for industrial oven; has semi-axial impeller enclosed directly by ninety degree deflector to guide volume flow from impeller radially away from impeller axis |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109214141A (en) * | 2018-11-20 | 2019-01-15 | 西华大学 | Rotating stall prediction method and device |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: SECO/WARWICK S.A., POLAND Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MAGIERA, RADOMIR;KRYLLOWICZ, WLADYSLAW;JOZWIK, KRZYSZTOF;AND OTHERS;REEL/FRAME:026769/0001 Effective date: 20100401 Owner name: POLITECHNIKA LODZKA, POLAND Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SECO/WARWICK S.A.;REEL/FRAME:026769/0051 Effective date: 20110601 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |